Nonlinear Flight Control Design for a STT Missile
- Author(s):
- Publication title:
- A collection of technical papers : AIAA Guidance, Navigation and Control Conference, Montreal, Canada 6-9 August 2001
- Title of ser.:
- AIAA Paper : AIAA Guidance Navigation and Control Conference
- Ser. no.:
- 2001
- Pub. Year:
- 2001
- Vol.:
- Pt. 1
- No.:
- 2001-4161
- Paper no.:
- AIAA-2001-4161
- Page(from):
- 732
- Page(to):
- 737
- Pages:
- 6
- Pub. info.:
- Reston, VA: American Institute of Aeronautics and Astronautics
- ISBN:
- 9781563474835 [1563474832]
- Language:
- English
- Call no.:
- A07400/014018
- Type:
- Technical Paper
Similar Items:
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Robust Analysis for Missile Lateral Acceleration Control Using Finite Inclusion Theorem
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
3
Technical Paper
Dynamic Inversion for Missile Lateral Velocity Control via Polynomial Eigenstructure Assignment
American Institute of Aeronautics and Astronautics |
9
Technical Paper
Earliest Intercept Line Guidance: A Novel Concept for Improving Mid-Course Guidance in Area Air Defence
American Institute of Aeronautics and Astronautics |
4
Technical Paper
Lateral Acceleration Controller for Missile via Polynomial Eigenstructure Assignment
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |